Gas Turbine Cooling Blades

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lows: 1.) Increase in turbine inlet temperature 2,) Use of regeneration 3.) Use of intercooling . of the idea of blade cooling. In these, blade cooling is generally presented as a means for making possible higher turbine inlet temperature and correspondingly. all. Blade cooling is to be considered in this thesis as a means of improving the thermal efficiency of the gas turbine by permitting the use of increased turbine inlet temperature. The improvement obtained in this.

. in a simple way describe a new and advanced cooling technology. The cooling technology described under the introduction below is a combination of traditional film-, impingement- and pin cooling. The only parameter that has been considered is the film cooling efficiency η , and no concern to heat transfer between the .

. in a simple way describe a new and advanced cooling technology. The cooling technology described under the introduction below is a combination of traditional film-, impingement- and pin cooling. The only parameter that has been considered is the film cooling efficiency η , and no concern to heat transfer between the .

. convection cooling of gas turbine blades and vanes is demonstrated in a test facility designed to simulate the first-stage turbine blade of the AGT 1500 gas turbine engine which powers the Army's M1 Abrams Main Battle Tank. A cylindrical test section is convectively cooled while.